On the reservoir quantity indicator 1834GQ:
-
the needle of the reservoir quantityindicator shows the contents of the Blue reservoir.
-there are no leaks from the pipe connection at the port marked B of the manual selector valve.
NOTE : When the hand pump is operated between 5 and 10 strokes, a small
____ quantity of fluid (between 200 and 400 ml) will go into the selected reservoir.
4.
Do the steps 2 and 3 again for The same result as in the steps 2 and the Yellow system. 3, for the Yellow reservoir.
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
5.
Do the steps 2 and 3 again for The same result as in the steps 2 and the Green system. 3, for the Green reservoir.
6.
On the manual selector valve On the reservoir quantity indicator 1134GQ: 1834GQ:
-set the selector switch of the - the Green indicator light goes off. manual selector valve to - the needle of the reservoir quantity NEUTRAL. indicator does not show the reservoir
contents.
5. Close-up
________
Subtask 29-16-51-860-051
A. Put the aircraft back to the serviceable condition.
(1)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
(2)
Disconnect the flexible hose from the fill valve 1698GM.
(3)
Put the flexible hose in its position in the ground service panel of the Green system.
(4)
Install the blanking cap on the fill valve 1698GM.
(5)
Remove the hand pump lever from the hand pump 1009GM.
(6)
Put the hand pump lever in position on the ground service panel of the Yellow system.
(7)
Remove the container from below the hydraulic connections.
(8)
Pressurize the reservoirs of the hydraulic systems.
(Ref. TASK 29-14-00-614-002).
(9)
Remove the access platform from below the ground service panel of the Green hydraulic system.
(10) Remove the warning notice(s).
Subtask 29-16-51-410-050
B. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install the access panel 197BB.
(3)
Close the access door 198CB.
SEAL DRAIN SYSTEM - DESCRIPTION AND OPERATION
_____________________________________________
1. General
_______
The seal drain system collects hydraulic fluid from the seal drains of specified components of the three hydraulic systems. The air relief valves of the reservoirs are also connected to the seal drain system. This is to collect any fluid which comes out of a reservoir if the pressure in the reservoir is too high. The fluid from a given component goes through a system of pipes to one of the two collector tanks. The tanks are the FWD collector tank and the AFT collector tank.
The system also gives some protection if the reservoirs are overfilled. However, if there is an excessive flow of fluid, or if the collector tank is full, the fluid comes out of the overflow pipe. In this case the fluid is not contained and goes into the hydraulic compartment.
2. Component Location
__________________
(Ref. Fig. 001)
-------------------------------------------------------------------------------FIN I FUNCTIONAL DESIGNATION I PANELIZONEIACCESS I ATA I I I IDOOR I REF.
-------------------------------------------------------------------------------TANK, COLLECTOR 196 196BB 29-17-41 TANK, COLLECTOR 148 29-17-41
3. System Description
__________________
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 002)
R **ON A/C 151-199, 301-399, 401-499,
(Ref. Fig. 002A)
**ON A/C ALL
The seal drain system has two plastic collector tanks (FWD and AFT) with related pipes and hoses. Each collector tank has a capacity of 0.75 l (0.1981 USgal) . Remove the hydraulic fluid from the collector tanks at regular times. The collector tanks are attached to the structure with quick release clamps to make them easier to drain.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM HYDRAULIC POWER 液压5(63)